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本文给出了惯性平台制导系统工作过程中,平台的回转方程与火箭的飞行姿态方程。方程中考虑了惯性制导系统的各种工具误差,可在弹道计算与制导飞行的精确描述中使用。本文还给出了方程的简化形式。介绍了在惯性制导的不同领域内使用这种方程的方法,叙述了星光-惯性制导的弹道跟踪方案及其实现方法以及星光自动瞄准的设想。
In this paper, the inertial platform guidance system working process, the platform of the rotation equation and the rocket flight attitude equation. The equations take into account the various tool errors of inertial guidance systems and can be used in the precise description of ballistic calculations and guided flights. This article also gives a simplified form of the equation. The method of using this equation in different fields of inertial guidance is introduced. The star - inertial guidance trajectory tracking scheme and its realization method and the idea of star automatic targeting are described.